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Unbolted in Fairfield (Update on the 2022 Bell 407 GXP Crash)

Fear of Landing

Then he followed the installation procedure, including the mast nut torque application. The mast nut torque application is a critical procedure, which ensures that the rotor assembly remains attached to the main rotor mast. He asked a mechanic to come and verify the mast nut torque.

Torque 89
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The Fenestron Factor: Cabri G2 Crash in Gruyéres

Fear of Landing

The pilot lowered the collective lever by 50%, which decreases the pitch angle of the main rotor blades and thus reduces the lift generated by the rotor. Reducing the lift and decreasing the torque effect helped to stabilize the helicopter. The helicopter, still powered, briefly lifted off again.

Rudder 107
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Overcoming the Five Most Common Landing Errors

Flight Training Central

It may be necessary to add a slight amount of power to keep the airspeed from decreasing excessively and to avoid losing lift too rapidly. By adding power, thrust can be increased to keep the airspeed from decelerating too rapidly and the wings from suddenly losing lift, but throttle must be closed immediately after touchdown.

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Is Flying a Helicopter Harder Than Flying a Plane? A Comparative Analysis

Pilot's Life Blog

Aerodynamic Differences Fixed-Wing Aircraft (Airplanes) Airplanes , or fixed-wing aircraft, generate lift through their stationary wings as they move forward. This pressure difference produces lift, allowing the aircraft to ascend. Each rotor blade acts as an airfoil, and as it rotates, it moves air over its surface, generating lift.

Torque 52
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Mastering Stalls: How to Recognize, Prevent, and Recover Safely

Flight Training Central

If the bank increases, the loss of vertical lift component tends to lower the nose. Because of engine torque and “P” factor, turns to the left will tend to steepen, and banks to the right tend to decrease. Then, slowly and smoothly bring the nose up to the attitude which will stall the airplane.

Rudder 93
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What Every Pilot Needs to Know about the Airplane Rudder

Northstar VFR

As air flows over it, a force like lift results, and the tail is pulled in the opposite direction of the deflection. But instead of an upward force of lift on a wing, it’s a horizontal force pushing the tail of the plane causing the nose of the plane to move left and right. Why is this? This is called adverse yaw.

Rudder 52
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When Push Comes to Shove

Plane and Pilot

We tried lifting the rear of the floats to increase the buoyancy offered by the larger front float chambers. The airplane began to torque to the left, and I was just about to pull the power to idle before the left wing hit the nearby tree when the left float let go, and we jumped forward into deeper water.